A nosecone apparatus for hypersonic aircraft, rocket or missiles using a method for the mitigation of the created the shock front of a rocket or aerospace plane flying at hypersonic speeds by using nosecone splines to create both centripetal and isentropic airflows in conjunction with regeneratively cooling the nosecone structure.


    Access

    Download


    Export, share and cite



    Title :

    System, apparatus and methods for a nosecone and a propulsive nozzle


    Contributors:

    Publication date :

    2020-09-22


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64G Raumfahrt , COSMONAUTICS / F25D REFRIGERATORS , Kühlschränke / F42B EXPLOSIVE CHARGES, e.g. FOR BLASTING , Explosive Ladungen, z.B. für Sprengungen



    System, apparatus, and methods for a nosecone and propulsive nozzle

    JANEKE CHARL E | European Patent Office | 2023

    Free access

    System, Apparatus and Methods for a Nosecone and a Propulsive Nozzle of an Airspace Plane

    JANEKE CHARL EMELIO | European Patent Office | 2017

    Free access

    System, apparatus and methods for a nosecone and a propulsive nozzle of an airspace plane

    JANEKE CHARL EMELIO | European Patent Office | 2019

    Free access

    Apparatus and Methods for Hypersonic Nosecone

    JANEKE CHARL E | European Patent Office | 2015

    Free access

    NOSECONE FOR AIRCRAFT

    KO MYUNG SANG / KIM JI HWAN / LEE CHANG MIN et al. | European Patent Office | 2020

    Free access